杨超, 邱祈生, 周宜涛, 吴志刚
CJA
收稿日期:2022-04-30
修回日期:2022-06-01
发布日期:2022-10-12
通讯作者:
吴志刚,E-mail:wuzhigang@buaa.edu.cn
E-mail:wuzhigang@buaa.edu.cn
YANG Chao, QIU Qisheng, ZHOU Yitao, WU Zhigang
Received:2022-04-30
Revised:2022-06-01
Published:2022-10-12
摘要： 为降低阵风对飞机飞行性能与安全的影响，早期往往通过加强飞机结构来抵抗阵风干扰。从20世纪50年代开始，人们逐步发展了基于主动控制的阵风响应减缓技术，并成功应用于多个实际飞机型号，有效降低了阵风响应，提高了飞机的疲劳寿命和飞行品质。国内的相关研究起步较晚，在国产大飞机等项目的需求牵引下，阵风减缓的工程应用已提上日程。本文提出了飞机阵风减缓研究的总体技术路线，并按此路线梳理了以下技术的历史发展和研究现状：首先介绍了阵风减缓的基础数学模型，涉及飞机动力学模型、阵风模型、非定常气动力模型及阵风响应分析方法；其次从减缓控制机理和控制律设计两个方面分析了阵风减缓的设计方法；回顾了阵风减缓风洞试验和飞行试验及实际应用的具体案例；最后概述了阵风减缓研究的前沿进展并总结了亟需解决的关键技术问题，以期为该领域的科研和工程技术人员提供借鉴与帮助。
中图分类号:
杨超, 邱祈生, 周宜涛, 吴志刚. 飞机阵风响应减缓技术综述[J]. 航空学报, 2022, 43(10): 527350-527350.
YANG Chao, QIU Qisheng, ZHOU Yitao, WU Zhigang. Review of aircraft gust alleviation technology[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(10): 527350-527350.
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